ACCESSORY GEARBOX ASSEMBLY FOR AN AIRCRAFT TURBINE ENGINE
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
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N/A
Issued Date -
N/A
app pub date -
Jan 16, 2015
filing date -
Jan 16, 2014
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
The invention relates to an accessory gearbox assembly for an aircraft turbine engine including: —a radial drive shaft (41); —an input gearbox (20) including an input gear, attachable onto a drive shaft (12) connecting a turbine (11) to a compressor (10) of the turbine engine, and an output gear secured to the radial drive shaft (41); —an accessory (51) including a stator, attachable to a housing (2) of the turbine engine, and a rotor that is rotatably mounted relative to the stator; and —a transfer gearbox (41) including an input gear, rotatably secured to the radial drive shaft (41), and an output gear rotatably secured to the rotor of the accessory (51). The input gear (45) engages with the output gear (46) so that, when the drive shaft (12) is rotated, the drive shaft rotates the rotor of the accessory (51) via the input gearbox (20), the radial drive shaft (41), and the transfer gearbox (41).
First Claim
Other Claims data not available